| dbo:abstract |
Der Avia Rk-17 ist ein Flugmotor des tschechoslowakischen Herstellers Avia aus dem Jahr 1934. Er ist die um zwei Zylinder vergrößerte Variante des Siebenzylindermotors Rk-12 (de) The Avia Rk.17 was a 9-cylinder radial aircraft engine, developed from the 7-cylinder Avia Rk.12, with a rated output of 270 kW (360 hp). The Rk.17 was one of Avia's own designs and was built in Czechoslovakia in the 1930s. (en) |
| dbo:thumbnail |
wiki-commons:Special:FilePath/Letecké_muzeum_Kbely_(39).jpg?width=300 |
| dbo:wikiPageID |
30087889 (xsd:integer) |
| dbo:wikiPageLength |
4284 (xsd:nonNegativeInteger) |
| dbo:wikiPageRevisionID |
997260839 (xsd:integer) |
| dbo:wikiPageWikiLink |
dbr:Prague dbr:Radial_engine dbr:Y_alloy dbr:Prague_Aviation_Museum,_Kbely dbr:Letov_Š-50 dbr:Supercharger dbr:Avia dbr:Czechoslovakia dbr:Hispano-Suiza dbr:Lorraine-Dietrich dbr:Power_rating dbr:Crankcase dbr:Crankshaft dbc:Aircraft_air-cooled_radial_piston_engines dbc:1930s_aircraft_piston_engines dbr:Avia_B.122 dbr:Avia_Rk.12 dbr:Piston dbr:Piston_rod dbr:Master_rod |
| dbp:bore |
130.0 |
| dbp:compression |
6.400000 (xsd:double) |
| dbp:coolingsystem |
air-cooled (en) |
| dbp:diameter |
1184.0 |
| dbp:displacement |
16.72 |
| dbp:fuelsystem |
single barrel Stromberg NAR80G carburettor * Ignition system: Scintilla magnetos, automatic advance (en) |
| dbp:fueltype |
petrol, 85 Octane (en) |
| dbp:length |
1065.0 |
| dbp:manufacturer |
dbr:Prague dbr:Avia |
| dbp:nationalOrigin |
dbr:Czechoslovakia |
| dbp:oilcon |
8.700000 (xsd:double) |
| dbp:oilsystem |
dry sump, with one pressure and one scavenging pump (en) |
| dbp:power |
165000.0 |
| dbp:reductionGear |
direct drive (en) |
| dbp:ref |
Jane's All the World's Aircraft 1938 (en) |
| dbp:specfuelcon |
255 (xsd:integer) |
| dbp:stroke |
140.0 |
| dbp:supercharger |
impeller drive ratio 10.7:1 (en) |
| dbp:type |
9 (xsd:integer) |
| dbp:valvetrain |
one inlet and one exhaust valve per cylinder, operated by push-rods via rocker gear. Eight cam push-rod disc drive. (en) |
| dbp:weight |
260 (xsd:integer) |
| dbp:wikiPageUsesTemplate |
dbt:Cite_book dbt:Commons_category dbt:Reflist dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Pistonspecs dbt:Avia_aeroengines |
| dcterms:subject |
dbc:Aircraft_air-cooled_radial_piston_engines dbc:1930s_aircraft_piston_engines |
| gold:hypernym |
dbr:Engine |
| rdf:type |
dbo:Software yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:HeatEngine103507963 yago:Instrumentality103575240 yago:Internal-combustionEngine103579982 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:RadialEngine104040373 yago:Whole100003553 yago:WikicatRadialEngines |
| rdfs:comment |
Der Avia Rk-17 ist ein Flugmotor des tschechoslowakischen Herstellers Avia aus dem Jahr 1934. Er ist die um zwei Zylinder vergrößerte Variante des Siebenzylindermotors Rk-12 (de) The Avia Rk.17 was a 9-cylinder radial aircraft engine, developed from the 7-cylinder Avia Rk.12, with a rated output of 270 kW (360 hp). The Rk.17 was one of Avia's own designs and was built in Czechoslovakia in the 1930s. (en) |
| rdfs:label |
Avia Rk-17 (de) Avia Rk.17 (en) |
| owl:sameAs |
freebase:Avia Rk.17 yago-res:Avia Rk.17 wikidata:Avia Rk.17 dbpedia-de:Avia Rk.17 http://tg.dbpedia.org/resource/Avia_Rk.17 https://global.dbpedia.org/id/4U8qz |
| prov:wasDerivedFrom |
wikipedia-en:Avia_Rk.17?oldid=997260839&ns=0 |
| foaf:depiction |
wiki-commons:Special:FilePath/Letecké_muzeum_Kbely_(39).jpg |
| foaf:isPrimaryTopicOf |
wikipedia-en:Avia_Rk.17 |
| is dbo:wikiPageWikiLink of |
dbr:Praga_E-51 dbr:List_of_aircraft_engines dbr:Jacobs_R-915 dbr:Armstrong_Siddeley_Cheetah dbr:Letov_Š-50 dbr:Bristol_Neptune dbr:Avia_B-158 dbr:Piaggio_Stella_P.VII |
| is dbp:eng1Name of |
dbr:Letov_Š-50 |
| is foaf:primaryTopic of |
wikipedia-en:Avia_Rk.17 |
